One-Dimensional Two-Phase Constant Lag Flow in Combustion Chamber of Solid Propellant Rocket Motors,

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Document Details

Document Type
Technical Report
Publication Date
Aug 15, 1984
Accession Number
ADA145679

Entities

People

  • C. Hsien'ch'i

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Burning Rate
  • Chambers
  • Combustion
  • Combustion Chambers
  • Engines
  • Equations
  • Equations Of State
  • Flow
  • Flow Fields
  • Foreign Technology
  • Propellants
  • Rocket Engines
  • Rockets
  • Solid Propellant Rocket Engines
  • Solid Propellants
  • Specific Heat
  • Two Phase Flow